FIELD: aviation.
SUBSTANCE: invention relates to a method for preventing an aircraft from getting into a dangerous zone of a vortex track of a vortex generator. To do this, information about the configuration, location and orientation of the aircraft at the current time, information about the position, geometric and mass characteristics and movement parameters of the vortex generator at the current time, information about the environmental parameters in the area of the aircraft and the vortex generator at the current time is received, geometric characteristics of the dangerous zone of the vortex track are determined in a certain way, visual information is provided to an aircraft crew about the risk of getting into the dangerous zone of the vortex track.
EFFECT: safety of the aircraft landing is ensured.
3 cl, 2 dwg
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